EP1466780A2 - Blockiermechanismus für Flugzeugdrehsitz - Google Patents

Blockiermechanismus für Flugzeugdrehsitz Download PDF

Info

Publication number
EP1466780A2
EP1466780A2 EP04008245A EP04008245A EP1466780A2 EP 1466780 A2 EP1466780 A2 EP 1466780A2 EP 04008245 A EP04008245 A EP 04008245A EP 04008245 A EP04008245 A EP 04008245A EP 1466780 A2 EP1466780 A2 EP 1466780A2
Authority
EP
European Patent Office
Prior art keywords
caliper
circular member
cable
braking
coupled
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP04008245A
Other languages
English (en)
French (fr)
Other versions
EP1466780B1 (de
EP1466780A3 (de
Inventor
George T. Beatty
Nathan A. Hemmer
John H. Traube
Carl R. Hutchison
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Goodrich Corp
Original Assignee
Decrane Aircraft Seating Co Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Decrane Aircraft Seating Co Inc filed Critical Decrane Aircraft Seating Co Inc
Publication of EP1466780A2 publication Critical patent/EP1466780A2/de
Publication of EP1466780A3 publication Critical patent/EP1466780A3/de
Application granted granted Critical
Publication of EP1466780B1 publication Critical patent/EP1466780B1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
    • B64D11/06—Arrangements of seats, or adaptations or details specially adapted for aircraft seats
    • B64D11/0639—Arrangements of seats, or adaptations or details specially adapted for aircraft seats with features for adjustment or converting of seats
    • B64D11/064—Adjustable inclination or position of seats
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60N—SEATS SPECIALLY ADAPTED FOR VEHICLES; VEHICLE PASSENGER ACCOMMODATION NOT OTHERWISE PROVIDED FOR
    • B60N2/00—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles
    • B60N2/02—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles the seat or part thereof being movable, e.g. adjustable
    • B60N2/04—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles the seat or part thereof being movable, e.g. adjustable the whole seat being movable
    • B60N2/06—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles the seat or part thereof being movable, e.g. adjustable the whole seat being movable slidable
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60N—SEATS SPECIALLY ADAPTED FOR VEHICLES; VEHICLE PASSENGER ACCOMMODATION NOT OTHERWISE PROVIDED FOR
    • B60N2/00—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles
    • B60N2/02—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles the seat or part thereof being movable, e.g. adjustable
    • B60N2/04—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles the seat or part thereof being movable, e.g. adjustable the whole seat being movable
    • B60N2/06—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles the seat or part thereof being movable, e.g. adjustable the whole seat being movable slidable
    • B60N2/062—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles the seat or part thereof being movable, e.g. adjustable the whole seat being movable slidable transversally slidable
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60N—SEATS SPECIALLY ADAPTED FOR VEHICLES; VEHICLE PASSENGER ACCOMMODATION NOT OTHERWISE PROVIDED FOR
    • B60N2/00—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles
    • B60N2/02—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles the seat or part thereof being movable, e.g. adjustable
    • B60N2/04—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles the seat or part thereof being movable, e.g. adjustable the whole seat being movable
    • B60N2/14—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles the seat or part thereof being movable, e.g. adjustable the whole seat being movable rotatable, e.g. to permit easy access
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60N—SEATS SPECIALLY ADAPTED FOR VEHICLES; VEHICLE PASSENGER ACCOMMODATION NOT OTHERWISE PROVIDED FOR
    • B60N2/00—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles
    • B60N2/90—Details or parts not otherwise provided for
    • B60N2/919—Positioning and locking mechanisms
    • B60N2/933—Positioning and locking mechanisms rotatable
    • B60N2/938—Positioning and locking mechanisms rotatable and provided with braking systems
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
    • B64D11/06—Arrangements of seats, or adaptations or details specially adapted for aircraft seats
    • B64D11/0649—Seats characterised by special features for reducing weight
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction

Definitions

  • the embodiments disclosed herein relate generally to brake systems, and more particularly to brake systems for adjustable seats.
  • RVs airplanes and recreational vehicles
  • Some seats permit a user to move the seat forward and backward, side-to-side, and around a central axis (e.g., rotational motion).
  • a central axis e.g., rotational motion
  • One system for controlling rotational movement includes using a disc or ring attached to a base assembly, which is attached to the floor of an airplane.
  • the disc or ring includes gear-like teeth disposed along the outer circumference of the disc'or ring.
  • a mating gear-like locking mechanism is attached to the seat, which can rotate freely when the user disengages the locking mechanism from the disc or ring.
  • the user engages'the locking mechanism, which permits a gear-like tooth to sit between one of the teeth disposed on the disc or ring.
  • the "gear" design has some drawbacks. For example, there are only a finite number of positions in which a user can securely position the seat. Depending on the width of the gear teeth, the angular distance between positions can be significant.
  • the seat can get stuck "between" teeth (e.g., locking mechanism not properly engaged between gear teeth). This can cause an undesirable situation in which the user incorrectly believes that the seat is locked. For example, in an airplane, a user holding a hot cup of coffee can be burned if a seat that is improperly "locked” jolts into a proper locked position when the airplane turns at a sharp angle or suddenly experiences turbulence.
  • the braking mechanism may comprise a circular member (e.g., a disc or ring) that is coupled to a base assembly and a caliper, coupled to a seat assembly, to engage the circular member.
  • a braking element of the caliper applies a braking force to the circular member.
  • a user can reduce the braking force by increasing the tension on a cable coupled to the caliper. Once the braking force is sufficiently reduced, the user may rotate the seat until the desired rotational orientation is attained. Upon release of the cable, the braking mechanism re-engages to prevent further rotational movement.
  • One alternative embodiment employs a band disposed around the circumference of the disc instead of a caliper. This embodiment may also employ a circumferential recess in the disc to ensure that the band remains engaged with the disc in both the biased and unbiased positions.
  • a brake shoe assembly is used to apply a braking force to a brake drum.
  • One or more brake shoes may be used to apply the braking force to at least one of an inner and an outer surface of the drum.
  • the braking system comprises a circular member and a braking mechanism to apply a braking force to the circular member.
  • the circular member can be a brake disc (e.g., solid structure) or ring (e.g., a disc with a substantial opening in the central portion of the disc).
  • the circular member shown in Figure 1 is brake ring 10.
  • a plurality of holes and/or grooves can be formed in the circular member.
  • the holes and grooves may be formed by any suitable technique such as, for example, drilling, milling, or molding.
  • brake ring 10 is coupled to swivel ring 12, which is coupled to base assembly 24 (shown in Figure 3).
  • Inner swivel 14 has bearings 16 (Figure 1) that can move within track 17 of swivel ring 12.
  • each bearing 16 only contacts track 17 at two points.
  • each bearing 16 may contact the upper edge of track 17 and the lower edge of track 17.
  • Such a configuration advantageously reduces friction between bearings 16 and track 17 to improve movement of inner swivel 14 relative to swivel ring 12.
  • Brake housing 18 is coupled to inner swivel 14 by brake bracket 19. This allows brake housing 18 to rotate with inner swivel 14 relative to brake ring 10 and swivel ring 12. In alternative embodiments, brake housing 18 remains stationary while brake ring 10 is capable of rotation.
  • brake housing 18 comprises a caliper with opening 20 to receive brake ring 10.
  • the caliper may include a first resilient member (e.g., an internal spring) to bias braking element 40 ( Figure 4) against at least one of a top side and a bottom side of brake ring 10. In this manner, the caliper is capable of applying a braking force to brake ring 10 via braking element 40.
  • a first resilient member e.g., an internal spring
  • Figure 3 shows an embodiment in which seat assembly 28 is coupled to inner swivel 14 (e.g., via linear bearing 26) so that seat 30 may be rotated relative to base assembly 24.
  • brake ring 10 remains stationary while inner swivel 14 and seat assembly 28 are capable of rotation.
  • cable 34 is provided to enable a user to reduce the braking force applied to the circular member (e.g., brake ring 10) such that seat assembly 28 may be rotated.
  • the proximal end of cable 34 may be attached to cable interface 22 of brake housing 18 ( Figures 3 and 4 ).
  • the distal end of cable 34 may be attached to brake handle 32 to permit a user to change the tension on cable 34 in order to effect a change in the amount of braking force applied to brake ring 10.
  • Brake handle 32 is coupled to arm rest 31 of seat 30.
  • the tension adjustment mechanism e.g., brake handle 32 or suitable alternative
  • the tension adjustment mechanism may be disposed in any suitable location.
  • Figure 4 shows an embodiment in which cable 34 is coupled (e.g., via cable interface 22) to the caliper to control the amount of braking force applied to brake ring 10.
  • the caliper comprises a resilient member (e.g., a spring disposed within brake housing 18) and braking element 40.
  • the connection between cable 34 and the caliper is such that a change in the tension of cable 34 can release the caliper from a biased position, in which braking element 40 is biased against the circular member disposed within opening 20 of the caliper.
  • the tension of cable 34 is increased to overcome the bias of the resilient member, the amount of force exerted on the circular member by braking element 40 is reduced to permit movement of seat assembly 28.
  • an adjustable resilient member e.g., spring 38
  • spring 38 can be used to adjust the amount of braking force exerted by the caliper in the biased position on the circular member.
  • spring 38 is disposed around cable interface 22 and has one end butted against (or coupled to) brake housing 18 and the other end coupled to stop 36.
  • Such a configuration is only one example of a mechanism for adjusting the braking force applied by the caliper in the biased position.
  • braking force can also be used to control movement in other directions (e.g., fore and aft movement, as well as transverse).
  • the braking mechanisms used to control movement in the other directions may work on the same or different principles as those disclosed herein.
  • Figure 5 shows one embodiment of a cable system that can actuate a plurality of braking mechanisms associated with the movement of a seat assembly.
  • tension splitter 42 may be coupled to cable 34 such that the tension applied by the user with handle 32 ( Figure 3 ) is divided among two or more cables (e.g. 44A, 44B, and 44C) to control different braking mechanisms.
  • cable 44A could be coupled to the braking mechanism to control fore and aft movement
  • cable 44B could be coupled to the braking mechanism to control transverse movement
  • cable 44C could be coupled to the braking mechanism to control rotational movement.
  • FIG. 3 shows one example of how base assembly 24 may be coupled to a portion of a vehicle (e.g., floor 23).
  • various embodiments may include a band that is disposed around the circumference of the disc (or ring) such that the band is biased to apply a frictional force to the disc to prevent rotational movement.
  • the disc may also have a circumferential recess in which the band is disposed. The recess helps the band remain engaged with the disc.
  • the user can actuate a cable to reduce to amount of braking force (e.g., friction) exerted on the disc. Similar to the other embodiments, the user may allow the cable to return to the biased position, in which the band tightens around the disc to prevent rotational movement.
  • a drum assembly may be used in place of a brake disc, and a brake shoe assembly may be used in place of a caliper.
  • at least one brake shoe is biased against the inner and/or the outer surface of the drum assembly.
  • various embodiments may include a cable to permit a user to reduce the braking force applied to the drum assembly, allowing the seat to rotate. Once the user has chosen a desired rotational orientation, the cable may be released so that the braking mechanism returns to the biased state in which the brake shoe assembly applies enough braking force to prevent rotational movement of the seat.

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transportation (AREA)
  • Mechanical Engineering (AREA)
  • Braking Arrangements (AREA)
EP04008245.5A 2003-04-07 2004-04-05 Blockiermechanismus für Flugzeugdrehsitz Expired - Lifetime EP1466780B1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US409976 1995-03-24
US10/409,976 US6938957B2 (en) 2003-04-07 2003-04-07 Rotation lock mechanism for aircraft seat

Related Child Applications (2)

Application Number Title Priority Date Filing Date
EP11004281.9 Division-Into 2011-05-24
EP11004425.2 Division-Into 2011-05-24

Publications (3)

Publication Number Publication Date
EP1466780A2 true EP1466780A2 (de) 2004-10-13
EP1466780A3 EP1466780A3 (de) 2008-07-09
EP1466780B1 EP1466780B1 (de) 2013-05-22

Family

ID=32869204

Family Applications (1)

Application Number Title Priority Date Filing Date
EP04008245.5A Expired - Lifetime EP1466780B1 (de) 2003-04-07 2004-04-05 Blockiermechanismus für Flugzeugdrehsitz

Country Status (2)

Country Link
US (1) US6938957B2 (de)
EP (1) EP1466780B1 (de)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102006013143A1 (de) * 2006-03-20 2007-09-27 Airbus Deutschland Gmbh Gastronomieabteil für ein Transportmittel für Passagiere
CN106427682A (zh) * 2016-11-24 2017-02-22 江苏忠明祥和精工股份有限公司 汽车座椅用转盘

Families Citing this family (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7600732B2 (en) * 2006-08-14 2009-10-13 Ami Industries, Inc. Aircraft interior equipment support
US8152101B2 (en) * 2006-09-12 2012-04-10 Law Sondra F System and method for integrating handicapped accessible seats into aircraft interior configurations
US7891629B2 (en) * 2006-11-02 2011-02-22 Labrador Development Llc Rotatable chair support
US7866751B2 (en) * 2007-10-02 2011-01-11 Brunswick Corporation Apparatus and methods to integrally form lever operated cables with vehicle seats
US7533930B1 (en) * 2007-10-24 2009-05-19 Embraer - Empresa Brasileira De Aeronautica S.A. Convertible aircraft passenger seat and method
EP2344408B1 (de) * 2008-09-22 2014-05-14 Crown Equipment Corporation Schwenkbarer sitz mit einstellbarem schwenkwiderstand
US9051053B2 (en) 2013-01-10 2015-06-09 Textron Innovations, Inc. Seat base for aircraft
US9428276B1 (en) 2015-02-19 2016-08-30 PAC Seating Systems, Inc. Swivel mechanism for vehicle seat
US10155591B2 (en) 2016-04-15 2018-12-18 Goodrich Corporation Rotational brake assembly for a seat locking mechanism
US10155590B2 (en) * 2016-04-15 2018-12-18 Goodrich Corporation Override bypass assembly for a seat locking mechanism
US9849813B2 (en) 2016-04-15 2017-12-26 Goodrich Corporation Carriage assembly for a seat locking mechanism
US9908446B2 (en) * 2016-04-15 2018-03-06 Goodrich Corporation Electric motor assembly for a seat locking mechanism
US20190038490A1 (en) * 2017-06-12 2019-02-07 Torrance D. Lillevold Rotational Transfer Platform System
CN107364797B (zh) * 2017-08-28 2018-09-11 沈阳安洋自控设备有限公司 一种联动台旋转底座
CN207725260U (zh) * 2017-11-28 2018-08-14 延锋安道拓座椅有限公司 一种锁止装置
US11110023B1 (en) * 2019-04-02 2021-09-07 Boyd Industries, Inc. Chair with swivel and brake system
US10994644B2 (en) * 2019-04-10 2021-05-04 B/E Aerospace, Inc. Lock mechanism for rotary component control
US10894495B2 (en) 2019-05-29 2021-01-19 Gulfstream Aerospace Corporation Seat assembly including an armrest with a lever handle and method for making the same
JP2022014373A (ja) * 2020-07-06 2022-01-19 トヨタ自動車株式会社 車両用シート及び車両
CN218327243U (zh) * 2022-04-15 2023-01-17 深圳市玛威尔显控科技有限公司 一种高稳定性的360度环拍平台
US20240253530A1 (en) * 2023-01-12 2024-08-01 Textron Aviation Inc. Swivel Locking System
US12427901B2 (en) * 2023-03-13 2025-09-30 Caterpillar Paving Products Inc. Plate and enclosure assembly for use in construction equipment
US12534208B2 (en) * 2023-08-02 2026-01-27 Textron Innovations Inc. Swivel indicating mechanism for aircraft seat
US12595064B2 (en) * 2023-10-03 2026-04-07 Textron Innovations Inc. Swivel locking mechanism for aircraft seat

Family Cites Families (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3622202A (en) * 1969-07-07 1971-11-23 Vernon C Brown Adjustable chair and control therefor
FI49708C (fi) * 1972-11-17 1975-09-10 Oulu Oy Menetelmä arvotuotteiden valmistamiseksi mäntypiestä.
US3858834A (en) * 1974-01-02 1975-01-07 Universal Oil Prod Co Locking mechanism for pedestal seat
US3926396A (en) 1974-06-12 1975-12-16 Universal Oil Prod Co Locking mechanism for pedestal seat
US4097016A (en) * 1977-05-12 1978-06-27 Danbar, Inc. Rotatable seat support assembly
US4671572A (en) * 1983-12-23 1987-06-09 Erda, Inc. Adjustable chair having roller cam adjustment mechanism
US4588226A (en) * 1983-12-23 1986-05-13 Erda, Inc. Adjustable chair for aircraft and the like
US4756502A (en) * 1986-06-26 1988-07-12 Nordam Aircraft seat
US4705256A (en) * 1986-07-23 1987-11-10 Seats, Inc. Swivel seat pedestal
US4893871A (en) * 1988-12-12 1990-01-16 Hickory Springs Manufacturing Co. Swivel rocker stop assembly
FR2684609B1 (fr) * 1991-12-10 1994-02-11 Faure Automobile Bertrand Base tournante a securite permettant la rotation de 180degre d'un siege dans un vehicule automobile ou analogue.
GB2301620B (en) * 1992-11-26 1997-07-02 Kab Seating Ltd Seats
DE4409841C2 (de) * 1993-06-04 2001-03-22 Honda Motor Co Ltd Raupen-Laufband für Raupenkraftfahrzeuge
CA2119341A1 (en) * 1993-08-13 1995-02-14 Vittorio Infanti Adjustable game stool assembly
US5634537A (en) 1995-04-19 1997-06-03 Lord Corporation Locking and positioning device
US5568960A (en) * 1995-09-15 1996-10-29 Aircraft Modular Products, Inc. Aircraft passenger seat swivel assembly
US5733006A (en) * 1996-05-02 1998-03-31 Sears Manufacturing Company Swivel seat suspension with free-swivel feature
EP0812722B1 (de) * 1996-06-14 2003-05-02 Ikeda Bussan Co., Ltd. Drehbare Vorrichtung für Kraftfahrzeugsitze
US5951106A (en) * 1996-09-13 1999-09-14 Ikeda Bussan Co., Ltd. Rotatable vehicle seat assembly with improved latching mechanism
JP3431773B2 (ja) * 1996-09-27 2003-07-28 アイシン精機株式会社 車両用回転式シート装置
US5904399A (en) * 1997-09-25 1999-05-18 Hanil Company Ltd. Rotary table of a seat for automobiles
US6116183A (en) * 1998-10-01 2000-09-12 Attwood Corporation Positively locking boat seat and method for making the same
US6361111B1 (en) * 1998-11-18 2002-03-26 Electric Mobility Corporation Rotational adjustment device
US6536842B2 (en) * 1998-11-18 2003-03-25 Electric Molorlity Corporation Rotational adjustment device
DE20006169U1 (de) * 2000-04-04 2001-08-09 Johnson Controls GmbH, 51399 Burscheid Vorrichtung zur Einstellung der Längsposition eines Fahrzeugsitzes
US6578854B2 (en) * 2001-07-30 2003-06-17 Solorider Industries, Inc. Personal mobility vehicle incorporating tilting and swiveling seat and method for use while playing golf

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102006013143A1 (de) * 2006-03-20 2007-09-27 Airbus Deutschland Gmbh Gastronomieabteil für ein Transportmittel für Passagiere
CN106427682A (zh) * 2016-11-24 2017-02-22 江苏忠明祥和精工股份有限公司 汽车座椅用转盘

Also Published As

Publication number Publication date
US6938957B2 (en) 2005-09-06
US20040195886A1 (en) 2004-10-07
EP1466780B1 (de) 2013-05-22
EP1466780A3 (de) 2008-07-09

Similar Documents

Publication Publication Date Title
US6938957B2 (en) Rotation lock mechanism for aircraft seat
US4466664A (en) Seat with a reclining back and an armrest
CA2246420C (en) Actuator that adjusts to side loads automatically by pivoting internally
CN111806697B (zh) 用于转动部件控制的锁定机构
US7296857B2 (en) Vehicle seat reclining device
US11766957B2 (en) Release mechanism for seat recliner assembly
US20130270884A1 (en) Recliner mechanism with dump feature
US20080030061A1 (en) Multi-position adjustment mechanism
US9994128B2 (en) Seat sliding device for vehicle
WO2002016162A1 (en) Compact disc recliner
US6267443B1 (en) Reclining seat for vehicle
CA2195088A1 (en) Infinitely adjustable linear actuator
EP1556243B1 (de) Vorrichtung zum verriegeln der konfiguration einer einrichtung,wie zum beispiel eines fahrzeugsitzes
CA2669168A1 (en) Customizable pedal system
US5556165A (en) Infinitely adjustable linear actuator for vehicle seat
US20050015929A1 (en) Braking system for braking a first element relative to a second element, and a vehicle seat including such a braking system
CN111806698B (zh) 转动靠背倾斜机构
US5607032A (en) Rotatable shaft lock apparatus
EP0425237A2 (de) Neigungsverstellvorrichtung für einen Kraftfahrzeugsitz
CA2812408C (en) Recliner mechanism with dump feature
CN220655180U (zh) 椅背前倾机构及座椅
EP3398805B1 (de) Gesicherte vorrichtung zum drehen eines sitzes, insbesondere für ein schienenfahrzeug
EP4436874A1 (de) Sicherheitsgurt-befestigungssystem für einen beweglichen sitz
JPH06296528A (ja) スプリングの予圧調整装置

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

AK Designated contracting states

Kind code of ref document: A2

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IT LI LU MC NL PL PT RO SE SI SK TR

AX Request for extension of the european patent

Extension state: AL HR LT LV MK

RIN1 Information on inventor provided before grant (corrected)

Inventor name: HUTCHISON, CARL R.

Inventor name: TRAUBE, JOHN H.

Inventor name: HEMMER, NATHAN A.

Inventor name: BEATTY, GEORGE T.

PUAL Search report despatched

Free format text: ORIGINAL CODE: 0009013

AK Designated contracting states

Kind code of ref document: A3

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IT LI LU MC NL PL PT RO SE SI SK TR

AX Request for extension of the european patent

Extension state: AL HR LT LV MK

17P Request for examination filed

Effective date: 20090108

AKX Designation fees paid

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IT LI LU MC NL PL PT RO SE SI SK TR

17Q First examination report despatched

Effective date: 20090514

RAP1 Party data changed (applicant data changed or rights of an application transferred)

Owner name: GOODRICH CORPORATION

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IT LI LU MC NL PL PT RO SE SI SK TR

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

REG Reference to a national code

Ref country code: AT

Ref legal event code: REF

Ref document number: 613031

Country of ref document: AT

Kind code of ref document: T

Effective date: 20130615

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 602004042156

Country of ref document: DE

Effective date: 20130711

REG Reference to a national code

Ref country code: AT

Ref legal event code: MK05

Ref document number: 613031

Country of ref document: AT

Kind code of ref document: T

Effective date: 20130522

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: GR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20130823

Ref country code: FI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20130522

Ref country code: PT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20130923

Ref country code: SI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20130522

Ref country code: ES

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20130902

Ref country code: SE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20130522

Ref country code: AT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20130522

REG Reference to a national code

Ref country code: NL

Ref legal event code: VDEP

Effective date: 20130522

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: BG

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20130822

Ref country code: PL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20130522

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: CZ

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20130522

Ref country code: BE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20130522

Ref country code: EE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20130522

Ref country code: DK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20130522

Ref country code: SK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20130522

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: RO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20130522

Ref country code: IT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20130522

Ref country code: NL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20130522

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

26N No opposition filed

Effective date: 20140225

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 602004042156

Country of ref document: DE

Effective date: 20140225

REG Reference to a national code

Ref country code: DE

Ref legal event code: R119

Ref document number: 602004042156

Country of ref document: DE

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MC

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20130522

Ref country code: LU

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140405

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 20140405

REG Reference to a national code

Ref country code: DE

Ref legal event code: R119

Ref document number: 602004042156

Country of ref document: DE

Effective date: 20141101

REG Reference to a national code

Ref country code: FR

Ref legal event code: ST

Effective date: 20141231

REG Reference to a national code

Ref country code: IE

Ref legal event code: MM4A

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: DE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20141101

Ref country code: CH

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20140430

Ref country code: LI

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20140430

Ref country code: GB

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20140405

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: FR

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20140430

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20140405

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: CY

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20130522

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: HU

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT; INVALID AB INITIO

Effective date: 20040405

Ref country code: TR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20130522